Calculation Reactivity Degree for Axial Low-Account Turbines with Small Emergence Angles of Nozzle Devices

Mikhail Yu. Fershalov; Andrey Yu. Fershalov; Juriy Yu. Fershalov

doi:10.4028/www.scientific.net/AMR.915-916.341

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Calculation Reactivity Degree for Axial Low-Account Turbines with Small Emergence Angles of Nozzle Devices

Abstract:

This paper presents the possibility of constructing a mathematical regression model for the reactivity degree of turbine stages (with the nozzle exit angles 5 ° ... 9 ° and a diameter of 0.17 m) depending on the constructed and model factors that have the greatest impact on the function value.